 A Zenit reentry capsule | |
| Names | Zenit 2-10 |
|---|---|
| Mission type | Optical imaging reconnaissance |
| COSPAR ID | 1963-012A |
| SATCAT no. | 571 |
| Mission duration | 10 days |
| Spacecraft properties | |
| Spacecraft type | Zenit-2 |
| Manufacturer | OKB-1 |
| Launch mass | 4730 kg[1] |
| Start of mission | |
| Launch date | 28 April 1963, 09:36:00 GMT |
| Rocket | Vostok-2 |
| Launch site | Baikonur 1/5 |
| Contractor | OKB-1 |
| End of mission | |
| Disposal | Recovered |
| Landing date | 8 May 1963 |
| Landing site | Steppe in Kazakhstan |
| Orbital parameters | |
| Reference system | Geocentric[2] |
| Regime | Low Earth |
| Perigee altitude | 194 km |
| Apogee altitude | 388 km |
| Inclination | 65.0° |
| Period | 90.4 minutes |
| Epoch | 28 April 1963 |
Zenit programme Zenit-2 | |
Kosmos 16 (Russian: Космос 16 meaning Cosmos 16) or Zenit-2 No.10 was a Soviet optical film-return reconnaissance satellite which was launched in 1963. A Zenit-2 satellite, Kosmos 16 was the tenth of eighty-one such spacecraft to be launched.[3][4]
- ^ Cite error: The named reference
Displaywas invoked but never defined (see the help page). - ^ Cite error: The named reference
Trajectorywas invoked but never defined (see the help page). - ^ Krebs, Gunter. "Zenit-2 (11F61)". Gunter's Space Page. Archived from the original on 31 December 2011. Retrieved 13 December 2013.
- ^ Wade, Mark. "Zenit-2". Encyclopedia Astronautica. Archived from the original on 23 May 2012. Retrieved 13 December 2013.